View from above orbital plane
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View from above satellite
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Ground track
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The orbit data is extracted from the following two-line orbital elements,
1 39770U 14029E 23334.92128106 .00052477 00000-0 29466-2 0 9990
2 39770 98.0024 108.4538 0004393 116.3819 243.7862 15.13122432517265
| Epoch (UTC): | 30 November 2023 22:06:38 |
| Eccentricity: | 0.0004393 |
| inclination: | 98.0024° |
| perigee height: | 523 km |
| apogee height: | 530 km |
| right ascension of ascending node: | 108.4538° |
| argument of perigee: | 116.3819° |
| revolutions per day: | 15.13122432 |
| mean anomaly at epoch: | 243.7862° |
| orbit number at epoch: | 51726 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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